[fltsim.0]
title=Piper Arrow-III G-BEOH
sim=Piper Arrow-III-T
model=
panel=FP
sound=
texture=G-BEOH
kb_checklists=Piper Arrow-III_check
kb_reference=Piper Arrow-III_ref
atc_id= 
ui_manufacturer=Piper
ui_type=Arrow-III-T
ui_variation=PA28RT G-BEOH
description=Flight dynamics derived from FS2004 Mooney Bravo, adapted by Rien Cornelissen to match Arrow-IV flight characteristics\n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.1]
title=Piper Arrow-III N15MZ
sim=Piper Arrow-III-T
model=
panel=FP
sound=
texture=N15MZ
kb_checklists=Piper Arrow-III_check
kb_reference=Piper Arrow-III_ref
atc_id=N15MZ
ui_manufacturer=Piper
ui_type=Arrow-III-T
ui_variation=PA28RT N15MZ
description=Flight dynamics derived from FS2004 Mooney Bravo, adapted by Rien Cornelissen to match Arrow-IV flight characteristics\n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=


[General]
performance=Engine 200 hp at 2,575 RPM,                        constant speed prop\nMaximum Speed at MSL          140 kts\n75% Power Cruise                     138 kts at 6,600 ft\nMax. Rate of Climb                    940 ft\/min at MSL,                                                     90 kts,2900 lbs\nMaximum Range\t               1100 nm\nService Ceiling                           20,000 ft\nFuel Capacity\t               72 U.S gal\nEmpty Weight                              1809 lbs  \nMax Gross Weight\t                2900 lbs\nSeating\t\t                 4\n
atc_type=Arrow
atc_model=P28RT
Category=airplane

[WEIGHT_AND_BALANCE]
empty_weight= 1807
max_gross_weight= 2900.0

reference_datum_position= 4.0, 0.0, 0.0
empty_weight_CG_position= -4.0, 0.0, 0.0

max_number_of_stations= 5
station_load.0=  220.0,  -4.350, -0.800, -0.045
station_load.1=  200.0,  -4.350,  0.800, -0.045
station_load.2=    0.0,  -6.600, -0.800, -0.045           //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=    0.0,  -6.600,  0.800, -0.045           //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=   10.0,  -9.0,    0.0,    0.0             //Baggage         Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI= 1400
empty_weight_roll_MOI= 1137
empty_weight_yaw_MOI= 2360
empty_weight_coupled_MOI= 0.0

[flight_tuning]
cruise_lift_scalar= 1.0
parasite_drag_scalar= 1.0
induced_drag_scalar= 1.0
elevator_effectiveness= 0.7
aileron_effectiveness= 1.0
rudder_effectiveness= 1.0
pitch_stability= 1.0
roll_stability= 1.0
yaw_stability= 1.0
elevator_trim_effectiveness= 1.0
aileron_trim_effectiveness= 1.0
rudder_trim_effectiveness= 0.5

[Flaps.0]
type= 1
span-outboard= 0.5
extending-time= 0.2
system_type= 0
damaging-speed= 0.0
blowout-speed= 0.0
lift_scalar= 1.0
drag_scalar= 1.0
pitch_scalar= 1.0
flaps-position.0= 0.0, 0.0
flaps-position.1= 12.7, 0.0
flaps-position.2= 25.3, 0.0
flaps-position.3= 38.0, 0.0

[piston_engine]
power_scalar=1.0
cylinder_displacement= 63
compression_ratio= 8.5
number_of_cylinders=6
max_rated_rpm= 2575
max_rated_hp= 200
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 1
turbocharged= 1
max_design_mp= 44
min_design_mp= 1
critical_altitude= 20000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.0
emergency_boost_gain_offset= 0.0
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.2
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=0.7

[propeller]
thrust_scalar=1.0
propeller_type= 0
propeller_diameter= 6.1
propeller_blades= 3
propeller_moi= 3
beta_max=38
beta_min= 15
min_gov_rpm= 1100
prop_tc= 0.1
gear_reduction_ratio= 1.0
fixed_pitch_beta= 0
low_speed_theory_limit= 80
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0
beta_feather= 0
power_absorbed_cf= 0
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0
minimum_reverse_beta= 0p

[pitot_static]
vertical_speed_time_constant= 0.7
pitot_heat=1.000000

[fuel]
LeftMain= -5.2, -6.500, 0.850, 36.0, 0.0
RightMain= -5.2, 6.500, 0.850, 36.0, 0.0
fuel_type= 1
number_of_tank_selectors= 1
electric_pump= 1

[airplane_geometry]
wing_area= 169.0
wing_span= 35.0
wing_root_chord= 5.3
wing_dihedral= 6.0
wing_incidence= 2.5
wing_twist= -1.5
oswald_efficiency_factor= 0.6
wing_winglets_flag= 0
wing_sweep= 15.0
wing_pos_apex_lon= 5.7
wing_pos_apex_vert= 1.314
htail_area= 39.0
htail_span= 13.0
htail_pos_lon= -19.3
htail_pos_vert= 5.0
htail_incidence= 2.0
htail_sweep= 0.0
vtail_area= 18.0
vtail_span= 4.8
vtail_sweep= 3.0
vtail_pos_lon= -18.5
vtail_pos_vert= 4.5
elevator_area= 35.0
aileron_area= 18.3
rudder_area= 6.7
elevator_up_limit= 28.0
elevator_down_limit= 21.0
aileron_up_limit= 20.0
aileron_down_limit= 15.0
rudder_limit= 24.0
elevator_trim_limit= 19.5
spoiler_limit= 0.0
spoilerons_available= 0
aileron_to_spoileron_gain= 0
min_ailerons_for_spoilerons= 0
min_flaps_for_spoilerons= 0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000

[contact_points]
//0  Class
//1  Longitudinal Position        (feet)
//2  Lateral Position             (feet)
//3  Vertical Position            (feet)
//4  Impact Damage Threshold      (Feet Per Minute)
//5  Brake Map                   (0=None, 1=Left, 2=Right)
//6  Wheel Radius                (feet)
//7  Steer Angle                  (degrees)
//8  Static Compression           (feet)  (0 if rigid)
//9  Max/Static Compression Ratio
//10 Damping Ratio               (0=Undamped, 1=Critically Damped)
//11 Extension Time              (seconds)
//12 Retraction Time             (seconds)
//13 Sound Type

point.0= 1.0,  1.866,  0.0, -2.95, 3500, 0, 0.500, 22.0, 0.250, 2.5, 0.90, 7.0, 7.0, 0
point.1= 1.0, -5.73, -5.14, -2.80, 3500, 1, 0.517, 0.0,  0.250, 2.5, 0.90, 7.0, 7.0, 2
point.2= 1.0, -5.73,  5.14, -2.80, 3500, 2, 0.517, 0.0,  0.250, 2.5, 0.90, 7.0, 7.0, 3

max_number_of_points= 21
static_pitch= 2.5
static_cg_height= 2.6
gear_system_type= 0

[GeneralEngineData]
engine_type= 0
Engine.0= 2.973, 0.400, 0.0
fuel_flow_scalar= 0.8
min_throttle_limit= 0.0

[Reference Speeds]
flaps_up_stall_speed= 58.0
full_flaps_stall_speed= 53.0
cruise_speed= 125.0
max_indicated_speed= 190

[keyboard_response]
elevator= 100.0, 180.0
aileron= 200.0, 1000.0
rudder= 200.0, 1000.0

[Views]
eyepoint= -5.64, -0.715, 2.08 //(feet) longitudinal, lateral, vertical distance from reference datum

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 500
default_bank_mode=1
autothrottle_available= 0
pitch_takeoff_ga= 8.0
use_no_default_bank= 0
use_no_default_pitch= 1
default_pitch_mode=0
default_bank_mode= 0
max_pitch= 10.00
max_pitch_acceleration= 1.0
max_pitch_velocity_lo_alt= 2.0
max_pitch_velocity_hi_alt= 1.5
max_pitch_velocity_lo_alt_breakpoint= 20000
max_pitch_velocity_hi_alt_breakpoint= 28000
max_bank= 20.00
max_bank_acceleration= 3.0
max_bank_velocity= 5.0
max_throttle_rate= 0.10
nav_proportional_control= 9.0
nav_integrator_control= 0.25
nav_derivative_control= 0.00
nav_integrator_boundary= 2.5
nav_derivative_boundary= 0.0
gs_proportional_control= 9.5
gs_integrator_control= 0.26
gs_derivative_control= 0.0
gs_integrator_boundary= 0.7
gs_derivative_boundary= 0.0
yaw_damper_gain= 0.0

[direction_indicators]
direction_indicator.0= 1, 0

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

flap_motor= 0, 5 , 17.0
gear_motor= 0, 5 , 17.0
autopilot= 0, 5 , 17.0
avionics_bus= 0, 5 , 17.0
avionics= 1, 5 , 17.0
pitot_heat= 0, 2 , 17.0
additional_system= 0, 2 , 17.0
marker_beacon= 1, 2 , 17.0
gear_warning= 0, 2 , 17.0
fuel_pump= 0, 5 , 17.0
starter1= 0, 20, 17.0
light_nav= 0, 5 , 17.0
light_beacon= 0, 5 , 17.0
light_landing= 0, 5 , 17.0
light_taxi= 0, 5 , 17.0
light_strobe= 0, 5 , 17.0
light_panel= 0, 5 , 17.0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1= 1
Com.1= 1, 1
Com.2= 1, 1
Nav.1= 1, 1, 1
Nav.2= 1, 1, 0
Adf.1= 1
Transponder.1= 1
Marker.1= 1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
//(feet) longitudinal, lateral, vertical distance from reference datum

light.0= 2,  -5.75, -17.0, 1.0, fx_strobeh
light.1= 2,  -5.75,  17.0, 1.0, fx_strobeh
light.2= 4,  -4.26, 0.0, 2.66, fx_vclight
light.3= 3, -5.572, -16.831, 0.972, fx_navred
light.4= 3, -5.572,  16.831, 0.972, fx_navgre
light.5= 1, -18.20,   0.00, 5.50, fx_beacon
light.6= 1, -18.20,   0.00, 5.40, fx_beacon

[exits]
number_of_exits= 2
exit_rate.0= 0.2

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[brakes]
toe_brakes_scale= 1.0
parking_brake= 1

[gear_warning_system]
gear_warning_available= 1
pct_throttle_limit= 50
flap_limit_power= 20
flap_limit_idle= 20

[hydraulic_system]
normal_pressure= 0.0

[stall_warning]
type= 1
stick_shaker=0

[attitude_indicators]
attitude_indicator.0= 1

[turn_indicators]
turn_indicator.0= 1,0

[forcefeedback]
gear_bump_nose_magnitude= 6000
gear_bump_nose_direction= 18000
gear_bump_nose_duration= 250000
gear_bump_left_magnitude= 6000
gear_bump_left_direction= 35500
gear_bump_left_duration= 250000
gear_bump_right_magnitude= 6000
gear_bump_right_direction= 00500
gear_bump_right_duration= 250000
ground_bumps_magnitude1= 3250
ground_bumps_angle1= 8900
ground_bumps_intercept1= 5.0 
ground_bumps_slope1= 0.48
ground_bumps_magnitude2= 750
ground_bumps_angle2= 9100  
ground_bumps_intercept2= 0.075
ground_bumps_slope2= 1.0
crash_magnitude1= 10000
crash_direction1= 01000
crash_magnitude2= 10000
crash_direction2= 9000
crash_period2= 75000
crash_duration2= 25000


[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0